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04-BS-6 · December 2014

Question 2 of 8: Stepped Shaft — Torsion

Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)

Notes on this paper

04-BS-6: Mechanics of Materials — National Exams, December 2014

3 hours duration. Closed book (one hand-written aid sheet permitted). Any FIVE of the eight questions constitute a complete paper; all eight are solved below as a complete study resource.

Reference texts: Hibbeler, Mechanics of Materials, 10th ed.; Beer, Johnston, DeWolf & Mazurek, Mechanics of Materials, 7th ed.; Gere & Goodno, Mechanics of Materials, 8th ed.

Question 2: Stepped Shaft — Torsion (20 marks)

Question text not reproduced: the examination questions are © Engineers and Geoscientists BC. Open the official past paper (linked at the top of this page) to read the question, then follow the worked solution below.

Given.

Segment ABd=30 mm, L=600 mm, TA=1000 N·m CW at A
Segment BCd=60 mm, L=1000 mm, TB=3500 N·m CW at B
Segment CDd=40 mm, L=400 mm, TC=7000 N·m CCW at C
MaterialAluminum, G=25 GPa, τyield=220 MPa
SupportFixed at D

Find. (a) the maximum shear stress in the shaft and its variation across the radius there; (b) the angle of twist at A relative to the fixed end D.

AB: d=30 mm, L=600 mmBC: d=60 mm, L=1000 mmCD: d=40 mm, L=400 mmABCD1000 N·m CW3500 N·m CW7000 N·m CCW
Stepped shaft A-B-C-D, fixed at D, with the three applied torques and each segment’s diameter/length.

Approach. Cut each segment and sum the applied torques between the free end A and the cut to get the internal torque; compute τ=Tr/J in each segment to find the maximum, then sum φ=TL/(GJ) segment-by-segment (fixed-end convention) for the total twist at A.

  1. Internal torques (CW positive, summing from the free end A inward): $$T_{AB}=1000\text{ N}\cdot\text{m},\quad T_{BC}=1000+3500=4500\text{ N}\cdot\text{m},\quad T_{CD}=4500-7000=-2500\text{ N}\cdot\text{m}$$ (CD carries 2500 N·m the opposite sense, since TC is CCW and outweighs A+B).
  2. Polar moments $J=\pi d^4/32$: $$J_{AB}=79522\text{ mm}^4,\quad J_{BC}=1272345\text{ mm}^4,\quad J_{CD}=251327\text{ mm}^4.$$
  3. Maximum shear stress in each segment, $\tau=T(d/2)/J$: $$\tau_{AB}=188.6\text{ MPa},\quad \tau_{BC}=106.1\text{ MPa},\quad \tau_{CD}=198.9\text{ MPa}.$$ The largest occurs in the narrower CD segment despite carrying the smallest internal torque, because its diameter is also small: $$\boxed{\tau_{max}=198.9\text{ MPa (in CD)}}$$ — below the 220 MPa yield, so the shaft does not yield. Across the radius, τ varies linearly from 0 at the centre to this value at the outer fibre, $\tau(\rho)=\tau_{max}\rho/(d/2)$.
  4. Angle of twist at A (sum of the three segment twists, each $\phi=TL/(GJ)$, algebraic sign preserved): $$\phi_A=\phi_{AB}+\phi_{BC}+\phi_{CD}=0.2841\text{ rad}$$ $$\boxed{\phi_A = 16.279^{\circ}\ \text{(same sense as the net CW torques)}}$$
QuantityValue
TAB, TBC, TCD1000, 4500, −2500 N·m
τAB, τBC, τCD188.6, 106.1, 198.9 MPa
Maximum shear stress198.9 MPa (segment CD)
Angle of twist at A0.2841 rad = 16.28°